US2668413A
(en)
*
|
1948-03-15 |
1954-02-09 |
James V Giliberty |
Gas turbine power plant with duplexed blading
|
US2721445A
(en)
*
|
1949-12-22 |
1955-10-25 |
James V Giliberty |
Aircraft propulsion plant of the propeller-jet turbine type
|
US2672726A
(en)
*
|
1950-09-19 |
1954-03-23 |
Bell Aircraft Corp |
Ducted fan jet aircraft engine
|
US2835332A
(en)
*
|
1955-10-20 |
1958-05-20 |
Vern K Fry |
Power drive suitable for airplanes and helicopters
|
US2914918A
(en)
*
|
1955-12-28 |
1959-12-01 |
Poly Ind Inc |
Gas turbine jet engine starter with serially-connected concentrically-arranged combustion chambers
|
US2937495A
(en)
*
|
1956-02-27 |
1960-05-24 |
Power Jets Res & Dev Ltd |
Gas turbine plant
|
DE1085718B
(de)
*
|
1958-11-26 |
1960-07-21 |
Daimler Benz Ag |
Gasturbinentriebwerk
|
US3818695A
(en)
*
|
1971-08-02 |
1974-06-25 |
Rylewski Eugeniusz |
Gas turbine
|
US3861139A
(en)
*
|
1973-02-12 |
1975-01-21 |
Gen Electric |
Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
|
AU3276397A
(en)
*
|
1996-06-28 |
1998-01-21 |
Hiroyasu Tanigawa |
Combined steam and gas turbine engine
|
US6397577B1
(en)
*
|
2001-04-02 |
2002-06-04 |
The United States Of America As Represented By The Secretary Of The Air Force |
Shaftless gas turbine engine spool
|
EP1825112B1
(en)
*
|
2004-12-01 |
2013-10-23 |
United Technologies Corporation |
Cantilevered tip turbine engine
|
EP1825177B1
(en)
|
2004-12-01 |
2012-01-25 |
United Technologies Corporation |
Inflatable bleed valve for turbine engine and method of controlling bleed air
|
US7854112B2
(en)
*
|
2004-12-01 |
2010-12-21 |
United Technologies Corporation |
Vectoring transition duct for turbine engine
|
EP1841959B1
(en)
*
|
2004-12-01 |
2012-05-09 |
United Technologies Corporation |
Balanced turbine rotor fan blade for a tip turbine engine
|
US20080219833A1
(en)
*
|
2004-12-01 |
2008-09-11 |
United Technologies Corporation |
Inducer for a Fan Blade of a Tip Turbine Engine
|
US7921635B2
(en)
*
|
2004-12-01 |
2011-04-12 |
United Technologies Corporation |
Peripheral combustor for tip turbine engine
|
EP1825113B1
(en)
*
|
2004-12-01 |
2012-10-24 |
United Technologies Corporation |
Counter-rotating gearbox for tip turbine engine
|
EP1819907A2
(en)
*
|
2004-12-01 |
2007-08-22 |
United Technologies Corporation |
Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
|
US8087885B2
(en)
*
|
2004-12-01 |
2012-01-03 |
United Technologies Corporation |
Stacked annular components for turbine engines
|
US8033092B2
(en)
*
|
2004-12-01 |
2011-10-11 |
United Technologies Corporation |
Tip turbine engine integral fan, combustor, and turbine case
|
DE602004031679D1
(de)
*
|
2004-12-01 |
2011-04-14 |
United Technologies Corp |
Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk
|
WO2006059969A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Counter-rotating compressor case and assembly method for tip turbine engine
|
US7980054B2
(en)
*
|
2004-12-01 |
2011-07-19 |
United Technologies Corporation |
Ejector cooling of outer case for tip turbine engine
|
DE602004029950D1
(de)
*
|
2004-12-01 |
2010-12-16 |
United Technologies Corp |
Enggekoppelte getriebeanordnung für einen spitzenturbinenmotor
|
DE602004031986D1
(de)
*
|
2004-12-01 |
2011-05-05 |
United Technologies Corp |
Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
|
WO2006059993A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine with multiple fan and turbine stages
|
US7631480B2
(en)
*
|
2004-12-01 |
2009-12-15 |
United Technologies Corporation |
Modular tip turbine engine
|
WO2006060013A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan rotor of a tip turbine engine
|
US8468795B2
(en)
|
2004-12-01 |
2013-06-25 |
United Technologies Corporation |
Diffuser aspiration for a tip turbine engine
|
WO2006059999A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
|
US7882695B2
(en)
|
2004-12-01 |
2011-02-08 |
United Technologies Corporation |
Turbine blow down starter for turbine engine
|
US7976273B2
(en)
*
|
2004-12-01 |
2011-07-12 |
United Technologies Corporation |
Tip turbine engine support structure
|
US8757959B2
(en)
*
|
2004-12-01 |
2014-06-24 |
United Technologies Corporation |
Tip turbine engine comprising a nonrotable compartment
|
WO2006059985A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Axial compressor for tip turbine engine
|
US20090169385A1
(en)
*
|
2004-12-01 |
2009-07-02 |
Suciu Gabriel L |
Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
|
DE602004016059D1
(de)
*
|
2004-12-01 |
2008-10-02 |
United Technologies Corp |
Tip-turbinentriebwerk mit wärmetauscher
|
DE602004016065D1
(de)
|
2004-12-01 |
2008-10-02 |
United Technologies Corp |
Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
|
DE602004018045D1
(de)
*
|
2004-12-01 |
2009-01-08 |
United Technologies Corp |
Gebläseschaufelanordnung für ein tip-turbinentriebwerk und montageverfahren
|
US8096753B2
(en)
*
|
2004-12-01 |
2012-01-17 |
United Technologies Corporation |
Tip turbine engine and operating method with reverse core airflow
|
WO2006059987A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Particle separator for tip turbine engine
|
US8024931B2
(en)
|
2004-12-01 |
2011-09-27 |
United Technologies Corporation |
Combustor for turbine engine
|
US8365511B2
(en)
*
|
2004-12-01 |
2013-02-05 |
United Technologies Corporation |
Tip turbine engine integral case, vane, mount and mixer
|
WO2006059970A2
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Turbine engine with differential gear driven fan and compressor
|
US8152469B2
(en)
|
2004-12-01 |
2012-04-10 |
United Technologies Corporation |
Annular turbine ring rotor
|
WO2006059994A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan-turbine rotor of a tip turbine engine
|
WO2006060010A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Compressor inlet guide vane for tip turbine engine and corresponding control method
|
EP1831530B1
(en)
*
|
2004-12-01 |
2009-02-25 |
United Technologies Corporation |
Compressor variable stage remote actuation for turbine engine
|
WO2006060009A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
|
EP1828573B1
(en)
*
|
2004-12-01 |
2010-06-16 |
United Technologies Corporation |
Hydraulic seal for a gearbox of a tip turbine engine
|
EP1831520B1
(en)
*
|
2004-12-01 |
2009-02-25 |
United Technologies Corporation |
Tip turbine engine and corresponding operating method
|
WO2006060006A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine non-metallic tailcone
|
EP1841960B1
(en)
*
|
2004-12-01 |
2011-05-25 |
United Technologies Corporation |
Starter generator system for a tip turbine engine
|
EP1825170B1
(en)
*
|
2004-12-01 |
2009-03-18 |
United Technologies Corporation |
Gearbox lubrication supply system for a tip turbine engine
|
US9109537B2
(en)
*
|
2004-12-04 |
2015-08-18 |
United Technologies Corporation |
Tip turbine single plane mount
|
US8192141B1
(en)
*
|
2007-04-05 |
2012-06-05 |
The United States Of America As Represented By The Secretary Of The Air Force |
Dual compression rotor
|
US8967945B2
(en)
|
2007-05-22 |
2015-03-03 |
United Technologies Corporation |
Individual inlet guide vane control for tip turbine engine
|
US8176725B2
(en)
*
|
2009-09-09 |
2012-05-15 |
United Technologies Corporation |
Reversed-flow core for a turbofan with a fan drive gear system
|
US20110146289A1
(en)
*
|
2009-12-21 |
2011-06-23 |
John Lewis Baughman |
Power extraction method
|
US20110146228A1
(en)
*
|
2009-12-21 |
2011-06-23 |
John Lewis Baughman |
Power extraction system
|
US20120324901A1
(en)
*
|
2011-06-23 |
2012-12-27 |
United Technologies Corporation |
Tandem fan-turbine rotor for a tip turbine engine
|
US9879694B2
(en)
|
2015-02-03 |
2018-01-30 |
United Technologies Corporation |
Turbo-compressor with geared turbofan
|
US10100731B2
(en)
*
|
2015-02-13 |
2018-10-16 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10337401B2
(en)
*
|
2015-02-13 |
2019-07-02 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10041408B2
(en)
*
|
2015-02-13 |
2018-08-07 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10125722B2
(en)
|
2015-02-13 |
2018-11-13 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10378438B2
(en)
*
|
2016-04-20 |
2019-08-13 |
Rolls-Royce North American Technologies, Inc. |
Reverse flow gas turbine engine with radially outward turbine
|
US10883424B2
(en)
|
2016-07-19 |
2021-01-05 |
Pratt & Whitney Canada Corp. |
Multi-spool gas turbine engine architecture
|
US11415063B2
(en)
|
2016-09-15 |
2022-08-16 |
Pratt & Whitney Canada Corp. |
Reverse-flow gas turbine engine
|
US10465611B2
(en)
|
2016-09-15 |
2019-11-05 |
Pratt & Whitney Canada Corp. |
Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
|
US11035293B2
(en)
|
2016-09-15 |
2021-06-15 |
Pratt & Whitney Canada Corp. |
Reverse flow gas turbine engine with offset RGB
|
US10815899B2
(en)
|
2016-11-15 |
2020-10-27 |
Pratt & Whitney Canada Corp. |
Gas turbine engine accessories arrangement
|
US10544734B2
(en)
*
|
2017-01-23 |
2020-01-28 |
General Electric Company |
Three spool gas turbine engine with interdigitated turbine section
|
US10539020B2
(en)
*
|
2017-01-23 |
2020-01-21 |
General Electric Company |
Two spool gas turbine engine with interdigitated turbine section
|
US10655537B2
(en)
*
|
2017-01-23 |
2020-05-19 |
General Electric Company |
Interdigitated counter rotating turbine system and method of operation
|
US10738709B2
(en)
|
2017-02-09 |
2020-08-11 |
Pratt & Whitney Canada Corp. |
Multi-spool gas turbine engine
|
US10808624B2
(en)
|
2017-02-09 |
2020-10-20 |
Pratt & Whitney Canada Corp. |
Turbine rotor with low over-speed requirements
|
US10215052B2
(en)
|
2017-03-14 |
2019-02-26 |
Pratt & Whitney Canada Corp. |
Inter-shaft bearing arrangement
|
US10746188B2
(en)
|
2017-03-14 |
2020-08-18 |
Pratt & Whitney Canada Corp. |
Inter-shaft bearing connected to a compressor boost system
|
US10718265B2
(en)
|
2017-05-25 |
2020-07-21 |
General Electric Company |
Interdigitated turbine engine air bearing and method of operation
|
US10669893B2
(en)
|
2017-05-25 |
2020-06-02 |
General Electric Company |
Air bearing and thermal management nozzle arrangement for interdigitated turbine engine
|
US10787931B2
(en)
|
2017-05-25 |
2020-09-29 |
General Electric Company |
Method and structure of interdigitated turbine engine thermal management
|
US10605168B2
(en)
|
2017-05-25 |
2020-03-31 |
General Electric Company |
Interdigitated turbine engine air bearing cooling structure and method of thermal management
|
US20190063313A1
(en)
*
|
2017-08-28 |
2019-02-28 |
Mustafa Rez |
Disc Turbine Engine
|
US10344763B2
(en)
*
|
2017-08-28 |
2019-07-09 |
Mustafa Rez |
Disc turbo charger
|
US11434831B2
(en)
|
2018-05-23 |
2022-09-06 |
General Electric Company |
Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
|
CN110529250B
(zh)
*
|
2018-05-23 |
2022-08-02 |
通用电气公司 |
燃气涡轮发动机
|
CN110821677A
(zh)
|
2018-08-08 |
2020-02-21 |
普拉特 - 惠特尼加拿大公司 |
多发动机系统和方法
|
US11255266B2
(en)
*
|
2019-05-14 |
2022-02-22 |
Raytheon Technologies Corporation |
Recuperated cycle engine
|
WO2021163760A1
(en)
*
|
2020-02-19 |
2021-08-26 |
Nathan Geoffrey Andrews |
A compact turbine-compressor assembly
|
US11428160B2
(en)
|
2020-12-31 |
2022-08-30 |
General Electric Company |
Gas turbine engine with interdigitated turbine and gear assembly
|